EP1832891B1 - Procédé et appareil de transformation d'overbounds - Google Patents
Procédé et appareil de transformation d'overbounds Download PDFInfo
- Publication number
- EP1832891B1 EP1832891B1 EP06004754.5A EP06004754A EP1832891B1 EP 1832891 B1 EP1832891 B1 EP 1832891B1 EP 06004754 A EP06004754 A EP 06004754A EP 1832891 B1 EP1832891 B1 EP 1832891B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- erf
- overbounding
- errors
- galileo
- overbounds
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000000034 method Methods 0.000 title claims description 14
- 230000001131 transforming effect Effects 0.000 title 1
- 238000013507 mapping Methods 0.000 description 13
- 238000009826 distribution Methods 0.000 description 12
- 101100228469 Caenorhabditis elegans exp-1 gene Proteins 0.000 description 5
- 230000003247 decreasing effect Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 230000009466 transformation Effects 0.000 description 2
- 101000972822 Homo sapiens Protein NipSnap homolog 2 Proteins 0.000 description 1
- 102100022564 Protein NipSnap homolog 2 Human genes 0.000 description 1
- 230000003416 augmentation Effects 0.000 description 1
- 238000005352 clarification Methods 0.000 description 1
- 238000005315 distribution function Methods 0.000 description 1
- 231100001261 hazardous Toxicity 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/13—Receivers
- G01S19/20—Integrity monitoring, fault detection or fault isolation of space segment
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/03—Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers
- G01S19/08—Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers providing integrity information, e.g. health of satellites or quality of ephemeris data
Definitions
- the invention relates to a procedure and an apparatus for transferring a Galileo overbound or an ICAO overbound to a pairwise overbound with excess mass (POEM).
- GNSS Global Navigation Satellite Systems
- HMI hazardously misleading information
- the integrity information sent to the user contains no explicit provisions for protecting against biases. Instead the user are sent protection factors that correspond to zero-mean error distributions.
- the users combine the received protection factors using their own local knowledge to calculate protection levels that correspond to their position estimate.
- the broadcast protection factors must be sufficient such that any individual user has only a small probability (e.g. less than a one in ten million), for each approach, that their true position error exceeds the calculated protection level.
- the ground system for instance must guarantee these protection factors without knowing precisely where the users are, or which satellite they observe.
- errors in the range domain are transformed into errors in the position domain.
- the corresponding error statistics probability distribution functions of the errors
- the Galileo overbounding As defined by the Galileo requirements.
- Another concept is the paired overbounding with excess mass (POEM).
- the Galileo overbounding has the disadvantage that it is not preserved during convolution, whereas the POEM is preserved during convolution. That means that the convolution of two excess mass overbounding distributions will overbound the convolution of the two original convolutions.
- the paired overbounding concept effectively relates range domain and position domain overbounding.
- This document describes how the Galileo Overbounding definition of a distribution can be used to define parameters for a paired overbounding with excess mass (POEM) of the same distribution. This is necessary as the properties of the Galileo overbounding definition are not preserved during convolutions of distributions, whereas the paired overbounding with excess mass properties are preserved during convolutions of distributions. The convolution is necessary for the transformation from the range domain to the position domain.
- the probability density p is overbounded by a function q if the equation ⁇ - ⁇ - y p x d x + ⁇ y ⁇ p x d x ⁇ ⁇ - ⁇ - y q x d y + ⁇ y ⁇ q x d x for all y ⁇ 0 holds true.
- a probability density p is paired overbounded by the functions q L and q R , if the equation ⁇ - ⁇ y q L x d x ⁇ ⁇ - ⁇ y p x d x ⁇ 1 - ⁇ y ⁇ q R x d x for all y holds true.
- the probability density p is overbounded by a function q if the equations ⁇ - ⁇ - y p x d x ⁇ ⁇ - ⁇ - y q x d y for all y ⁇ 0 ⁇ y ⁇ p x d x ⁇ ⁇ y ⁇ q x d y for all y ⁇ 0 hold true.
- the ICAO overbounding definition implies directly the Galileo overbounding definition. This can be seen by a simple addition of the defining inequalities. The opposite is not valid in general.
- ICAO overbounding implies Galileo overbounding. Therefore the method of mapping Galileo overbounding to POEM described in the chapter before is also applicable for ICAO overbounding.
- a positive function q L is part of POEM if inequality ⁇ - ⁇ y q L x d x ⁇ ⁇ - ⁇ y p x d x is fulfilled for all y .
- a positive function q R is part of POEM if inequality 1 - K R + ⁇ - ⁇ y q R x d x ⁇ ⁇ - ⁇ y p x d x is fulfilled for all y .
- the invention further discloses an apparatus that is arranged such that it is capable to execute the methods described above.
- Such an apparatus could be part of one of the GNSS, e.g. a satellite of the GNSS or some ground systems or the receiver of a user.
- the invention was described for GNSS and the overbounding concepts Galileo Overbounding, ICAO Overbounding and Paired Overbounding with Excess Mass. However, it is to be understood by those skilled in the art that the invention is neither limited to GNSS nor to Galileo Overbounding, ICAO Overbounding and Paired Overbounding with Excess Mass, respectively.
- ⁇ f t exp - t 2 ⁇ 0 z ⁇ f + ⁇ 0 ⁇ ⁇ f + erf z ⁇ ⁇ 0 ⁇ ⁇ f ⁇ ⁇ l ⁇ 0 z ⁇ - ⁇ ⁇ f
- (2) is equivalent to: - ⁇ ⁇ ⁇ z ⁇ f + erf z ⁇ ⁇ 0 ⁇ ⁇ f ⁇ ⁇ ! - ⁇ 0 ⁇ ⁇ - z ⁇ f .
- ⁇ erf z ⁇ - erf z ⁇ ⁇ 0 ⁇ ⁇ - z ⁇ f ⁇ ⁇ z ⁇ z ⁇ f + erf z ⁇ ⁇ 0 ⁇ ⁇ f .
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Computer Security & Cryptography (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
Claims (2)
- Procédé pour déterminer des bornes surestimées prudentes dans un système de positionnement par satellites, le procédé comprenant les étapes consistant à :- déterminer des bornes surestimées prudentes (qi(x)) d'au moins une erreur (εi) dans un domaine de distances,- multiplier séparément les bornes surestimées prudentes (qi(x)) d'erreurs (εi) dans le domaine de distances une fois par une première fonction θ(-x)·2 et une autre fois par une deuxième fonction θ(x)·2, θ(x) étant définie de la façon suivante : θ(x)=1 pour x≥0 et θ(x)=0 pour x<0, dans le but d'obtenir des paires de bornes surestimées prudentes (qiL(x) et (qiR(x)) d'erreurs (εi) dans le domaine de distances,- déterminer une borne supérieure pour le risque d'intégrité à la limite d'alerte (pw,int(AL)) dans un domaine de positions à partir de paires de bornes surestimées (qiL(x) et (qiR(x)) d'erreurs (εi) dans le domaine de distances.
- Appareil, conçu exécuter un procédé selon la revendication 1.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP06004754.5A EP1832891B1 (fr) | 2006-03-08 | 2006-03-08 | Procédé et appareil de transformation d'overbounds |
US11/683,195 US8849569B2 (en) | 2006-03-08 | 2007-03-07 | Method and apparatus for transforming overbounds |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP06004754.5A EP1832891B1 (fr) | 2006-03-08 | 2006-03-08 | Procédé et appareil de transformation d'overbounds |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1832891A1 EP1832891A1 (fr) | 2007-09-12 |
EP1832891B1 true EP1832891B1 (fr) | 2013-05-08 |
Family
ID=36940313
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP06004754.5A Active EP1832891B1 (fr) | 2006-03-08 | 2006-03-08 | Procédé et appareil de transformation d'overbounds |
Country Status (2)
Country | Link |
---|---|
US (1) | US8849569B2 (fr) |
EP (1) | EP1832891B1 (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8849569B2 (en) | 2006-03-08 | 2014-09-30 | Eads Astrium Gmbh | Method and apparatus for transforming overbounds |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2418513A1 (fr) * | 2010-08-10 | 2012-02-15 | Astrium GmbH | Calcul des paramètres de précision robustes et améliorés de signaux de satellite d'un système de navigation par satellite global ou régional |
EP2461182B1 (fr) * | 2010-12-01 | 2014-06-04 | European Space Agency | Procédé et appareil permettant de déterminer un paramètre d'indication d'intégrité indiquant l'intégrité des informations de positionnement déterminées dans un système global de positionnement |
WO2015131906A1 (fr) * | 2014-03-06 | 2015-09-11 | Weibel Scientific A/S | Estimation de distance par fréquences multiples |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102004059229A1 (de) * | 2004-12-08 | 2006-06-14 | Eads Astrium Gmbh | Fahrzeug-System sowie ein erdfestes Empfangseinrichtungs-System |
EP1832891B1 (fr) | 2006-03-08 | 2013-05-08 | EADS Astrium GmbH | Procédé et appareil de transformation d'overbounds |
US7733268B2 (en) * | 2006-05-16 | 2010-06-08 | Andrew Corporation | Method and apparatus for determining the geographic location of a device |
FR2903499B1 (fr) * | 2006-07-05 | 2008-08-22 | Alcatel Sa | Dispositif de generation de messages d'integrite signalant des stations de surveillance nominales, degradees ou inactives de systemes de navigation par satellites |
US7436354B2 (en) * | 2006-09-07 | 2008-10-14 | The Mitre Corporation | Methods and systems for mobile navigational applications using global navigation satellite systems |
US7847726B2 (en) * | 2006-12-22 | 2010-12-07 | Sirf Technology Holdings, Inc. | Navigational signal tracking in low power mode |
US7928903B2 (en) * | 2007-12-07 | 2011-04-19 | Andrew, Llc | Method and system for selecting optimal satellites for A-GPS location of handsets in wireless networks |
US8094072B2 (en) * | 2008-05-05 | 2012-01-10 | Qualcomm Incorporated | Adaptive coherent integration time |
-
2006
- 2006-03-08 EP EP06004754.5A patent/EP1832891B1/fr active Active
-
2007
- 2007-03-07 US US11/683,195 patent/US8849569B2/en active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8849569B2 (en) | 2006-03-08 | 2014-09-30 | Eads Astrium Gmbh | Method and apparatus for transforming overbounds |
Also Published As
Publication number | Publication date |
---|---|
EP1832891A1 (fr) | 2007-09-12 |
US8849569B2 (en) | 2014-09-30 |
US20070222669A1 (en) | 2007-09-27 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US6691066B1 (en) | Measurement fault detection | |
Blanch | Using Kriging to bound satellite ranging errors due to the ionosphere | |
EP2461182B1 (fr) | Procédé et appareil permettant de déterminer un paramètre d'indication d'intégrité indiquant l'intégrité des informations de positionnement déterminées dans un système global de positionnement | |
Li et al. | A procedure for the significance testing of unmodeled errors in GNSS observations | |
EP1832891B1 (fr) | Procédé et appareil de transformation d'overbounds | |
Khanafseh et al. | New approach for calculating position domain integrity risk for cycle resolution in carrier phase navigation systems | |
EP2037291A1 (fr) | Procédé de surveillance d'intégrité pour navigation GNSS basé sur des informations historiques | |
CN116075747A (zh) | 用于卫星定位的系统和方法 | |
Rife et al. | Formulation of a time-varying maximum allowable error for ground-based augmentation systems | |
Walter et al. | Vertical protection level equations for dual frequency SBAS | |
Ene et al. | Galileo-GPS RAIM for vertical guidance | |
Neri et al. | Integrity Bounds for Rail and Road Applications Based on Local Hazard Maps | |
Schempp et al. | An application of Gaussian overbounding for the WAAS fault free error analysis | |
EP2418513A1 (fr) | Calcul des paramètres de précision robustes et améliorés de signaux de satellite d'un système de navigation par satellite global ou régional | |
Pullen et al. | Integrity for non-aviation users | |
Blanch et al. | Advanced raim for mega-constellations | |
CN115598668A (zh) | 一种基于贝叶斯模型的完好性风险加速测试方法、装置、计算机及存储介质 | |
Khanafseh et al. | Integrity risk of cycle resolution in the presence of bounded faults | |
Altshuler et al. | Improvements to the WAAS ionospheric algorithms | |
Tossaint et al. | The stanford-ESA integrity diagram: focusing on SBAS integrity | |
Van Dyke et al. | GPS integrity failure modes and effects analysis | |
Margaria et al. | Proof-of-concept of the local integrity approach: Prototype implementation and performance assessment in an urban context | |
Chen et al. | Compass/BeiDou‐2 spaceborne clock performance assessment and its error detection, mitigation | |
Konno | Design of an aircraft landing system using dual-frequency GNSS | |
Pullen et al. | A new approach to GPS integrity monitoring using prior probability models and optimal threshold search |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR |
|
AX | Request for extension of the european patent |
Extension state: AL BA HR MK YU |
|
17P | Request for examination filed |
Effective date: 20080220 |
|
17Q | First examination report despatched |
Effective date: 20080320 |
|
AKX | Designation fees paid |
Designated state(s): DE FR GB IT |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R079 Ref document number: 602006036131 Country of ref document: DE Free format text: PREVIOUS MAIN CLASS: G01S0001000000 Ipc: G01S0019080000 |
|
RIC1 | Information provided on ipc code assigned before grant |
Ipc: G01S 19/20 20100101ALI20121004BHEP Ipc: G01S 19/08 20100101AFI20121004BHEP |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
RIN1 | Information on inventor provided before grant (corrected) |
Inventor name: TRAUTENBERG, HANS L., DR. Inventor name: FRANKENBERGER, HARALD, DR. |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): DE FR GB IT |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 602006036131 Country of ref document: DE Effective date: 20130704 |
|
RAP2 | Party data changed (patent owner data changed or rights of a patent transferred) |
Owner name: ASTRIUM GMBH |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R081 Ref document number: 602006036131 Country of ref document: DE Owner name: ASTRIUM GMBH, DE Free format text: FORMER OWNER: ASTRIUM GMBH, 81667 MUENCHEN, DE Effective date: 20130514 Ref country code: DE Ref legal event code: R081 Ref document number: 602006036131 Country of ref document: DE Owner name: ASTRIUM GMBH, DE Free format text: FORMER OWNER: EADS ASTRIUM GMBH, 81667 MUENCHEN, DE Effective date: 20130625 Ref country code: DE Ref legal event code: R081 Ref document number: 602006036131 Country of ref document: DE Owner name: AIRBUS DEFENCE AND SPACE GMBH, DE Free format text: FORMER OWNER: ASTRIUM GMBH, 81667 MUENCHEN, DE Effective date: 20130514 Ref country code: DE Ref legal event code: R081 Ref document number: 602006036131 Country of ref document: DE Owner name: AIRBUS DEFENCE AND SPACE GMBH, DE Free format text: FORMER OWNER: EADS ASTRIUM GMBH, 81667 MUENCHEN, DE Effective date: 20130625 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed |
Effective date: 20140211 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 602006036131 Country of ref document: DE Effective date: 20140211 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 11 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 12 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R081 Ref document number: 602006036131 Country of ref document: DE Owner name: AIRBUS DEFENCE AND SPACE GMBH, DE Free format text: FORMER OWNER: ASTRIUM GMBH, 82024 TAUFKIRCHEN, DE |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 13 |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: 732E Free format text: REGISTERED BETWEEN 20180405 AND 20180411 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: CD Owner name: AIRBUS DS GMBH, DE Effective date: 20180718 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20220321 Year of fee payment: 17 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: IT Payment date: 20220322 Year of fee payment: 17 Ref country code: FR Payment date: 20220322 Year of fee payment: 17 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20230321 Year of fee payment: 18 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20230308 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230308 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230308 Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230331 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230308 |